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NREL's S832 Airfoil (s832-nr)

NREL's S832 Airfoil - NREL HAWT airfoil S832


Airfoil s832-nr
Details Dat file Parser  
(s832-nr) NREL's S832 Airfoil
NREL HAWT airfoil S832
Max thickness 14.9% at 44% chord.
Max camber 5.3% at 44% chord
Source NWTC National WInd Technology Center
Source dat file
The dat file is in Selig format
NREL's S832 Airfoil
   x/c        y/c
1.000000   0.000000
0.996189   0.000690
0.985144   0.003330
0.967848   0.008395
0.945387   0.015755
0.918585   0.024881
0.887880   0.035169
0.853519   0.046383
0.816140   0.058387
0.776422   0.070791
0.734962   0.083121
0.692288   0.094860
0.648822   0.105440
0.604799   0.114365
0.560397   0.121287
0.515766   0.125985
0.471058   0.128305
0.426293   0.128244
0.381615   0.126142
0.337467   0.122329
0.294358   0.117013
0.252745   0.110366
0.213098   0.102561
0.175832   0.093763
0.141367   0.084153
0.110065   0.073902
0.082279   0.063197
0.058313   0.052175
0.038300   0.041018
0.022423   0.030004
0.010713   0.019421
0.003282   0.009733
0.000114   0.001503
0.000004   0.000278
0.000099  -0.001261
0.000264  -0.001935
0.000525  -0.002520
0.000941  -0.003030
0.001503  -0.003525
0.001881  -0.003804
0.002983  -0.004482
0.010744  -0.007277
0.025774  -0.009577
0.047344  -0.010877
0.075097  -0.011915
0.108254  -0.012945
0.146278  -0.014035
0.188463  -0.015224
0.234228  -0.016488
0.282871  -0.017793
0.333771  -0.019071
0.386222  -0.020247
0.439587  -0.021223
0.493169  -0.021885
0.546335  -0.022084
0.598428  -0.021585
0.649107  -0.020048
0.698213  -0.017446
0.745551  -0.013944
0.790900  -0.009907
0.833844  -0.005849
0.873785  -0.002344
0.909799   0.000129
0.940887   0.001438
0.966133   0.001687
0.984757   0.001184
0.996164   0.000414
1.000000   0.000000
Dat file parser warnings
  • Line 2 - Invalid characters : x/c y/c
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Polars for NREL's S832 Airfoil (s832-nr)

PlotAirfoilReynolds #NcritMax Cl/CdDescriptionSource 
   s832-nr50,000919.8 at α=13.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s832-nr50,000516 at α=13.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s832-nr100,000926.4 at α=12.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s832-nr100,000525.2 at α=11.75°Mach=0 Ncrit=5Xfoil predictionDetails
   s832-nr200,000954.7 at α=9.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s832-nr200,000567.2 at α=7°Mach=0 Ncrit=5Xfoil predictionDetails
   s832-nr500,0009126 at α=7.5°Mach=0 Ncrit=9Xfoil predictionDetails
   s832-nr500,0005118.9 at α=6.25°Mach=0 Ncrit=5Xfoil predictionDetails
   s832-nr1,000,0009163.3 at α=6.75°Mach=0 Ncrit=9Xfoil predictionDetails
   s832-nr1,000,0005151.2 at α=5.75°Mach=0 Ncrit=5Xfoil predictionDetails
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